![Turbocharger Systems and Methods for Operating the Same](/abs-image/US/2008/02/14/US20080034753A1/abs.jpg.150x150.jpg)
基本信息:
- 专利标题: Turbocharger Systems and Methods for Operating the Same
- 专利标题(中):涡轮增压器系统及其操作方法
- 申请号:US11464562 申请日:2006-08-15
- 公开(公告)号:US20080034753A1 公开(公告)日:2008-02-14
- 发明人: Anthony Holmes Furman , Shishir Chandrasekhar Menon , Kendall Roger Swenson , Daniel Edward Loringer
- 申请人: Anthony Holmes Furman , Shishir Chandrasekhar Menon , Kendall Roger Swenson , Daniel Edward Loringer
- 主分类号: F02B33/44
- IPC分类号: F02B33/44 ; F02D23/00
摘要:
Disclosed herein are turbocharger systems and methods for their operation. In one embodiment a turbocharger system is disclosed. The turbocharger system comprises a turbine, a compressor, an air inlet, a first sensor, a second sensor, and a controller. The turbine is mechanically connected to the compressor and the air inlet is connected in fluid communication to the compressor. The first sensor and the second sensor are connected in operational communication with the air inlet and disposed a sufficient distance from one another to be capable of measuring a temperature differential caused by a hot boundary layer. The controller is connected in operational communication with the first sensor and the second sensor, and the controller is configured to detect surge precursors.
摘要(中):
这里公开了涡轮增压器系统及其操作方法。 在一个实施例中,公开了一种涡轮增压器系统。 涡轮增压器系统包括涡轮机,压缩机,进气口,第一传感器,第二传感器和控制器。 涡轮机械地连接到压缩机,空气入口与压缩机流体连通地连接。 第一传感器和第二传感器与空气入口相连接地连接,并且彼此间设置足够的距离,以能够测量由热边界层引起的温差。 控制器与第一传感器和第二传感器的操作通信连接,并且控制器被配置为检测浪涌前兆。
IPC结构图谱:
F | 机械工程;照明;加热;武器;爆破 |
--F02 | 燃烧发动机;热气或燃烧生成物的发动机装置 |
----F02B | 活塞式内燃机;一般燃烧发动机 |
------F02B33/00 | 带有进气泵或扫气泵的发动机 |
--------F02B33/44 | .自泵至发动机进口的导料管,如贮气器 |